A Study on Heat Transfer Characteristics of Small Liquid Rocket Engine with Calorimeter
- 김종암
- Namkoung, Hyuck-Joon
- Han, Poong-Gyoo
- Kim, Hwa-Jung
- Lee, Kyoung-Hun
- Kim, Young-Soo
- Kim, Chongam
Publication date
July 2006
DOI Publisher
American Institute of Aeronautics and Astronautics (AIAA)Abstract
Small liquid rocket engine (SLRE) with calorimeter were developed and tested to evaluate cooling characteristics in the liquid rocket engine. Therefore, cooling performance analysis was performed to predict the heat transfer coefficient on gas side wall in 10 calorimeter channel. A heat transfer empirical formula was determined by results of firing test and computational simulation.OAIID:oai:osos.snu.ac.kr:snu2006-01/104/0000004648/34SEQ:34PERF_CD:SNU2006-01EVAL_ITEM_CD:104USER_ID:0000004648ADJUST_YN:NEMP_ID:A001138DEPT_CD:446CITE_RATE:0FILENAME:6.2006-5195.pdfDEPT_NM:기계항공공학부EMAIL:chongam@snu.ac.krCONFIRM:
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